EP0744541A1 - Procédé pour la production de blocs-moteurs - Google Patents

Procédé pour la production de blocs-moteurs Download PDF

Info

Publication number
EP0744541A1
EP0744541A1 EP96106912A EP96106912A EP0744541A1 EP 0744541 A1 EP0744541 A1 EP 0744541A1 EP 96106912 A EP96106912 A EP 96106912A EP 96106912 A EP96106912 A EP 96106912A EP 0744541 A1 EP0744541 A1 EP 0744541A1
Authority
EP
European Patent Office
Prior art keywords
cylinder
mold
liner assembly
liners
liner
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP96106912A
Other languages
German (de)
English (en)
Other versions
EP0744541B1 (fr
Inventor
Toshihiro Takami
Mitsuhiro Karaki
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyota Motor Corp
Original Assignee
Toyota Motor Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyota Motor Corp filed Critical Toyota Motor Corp
Publication of EP0744541A1 publication Critical patent/EP0744541A1/fr
Application granted granted Critical
Publication of EP0744541B1 publication Critical patent/EP0744541B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00—Casting in, on, or around objects which form part of the product
    • B22D19/0009—Cylinders, pistons
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00—Cylinders; Cylinder heads 
    • F02F1/02—Cylinders; Cylinder heads  having cooling means
    • F02F1/10—Cylinders; Cylinder heads  having cooling means for liquid cooling
    • F02F1/108—Siamese-type cylinders, i.e. cylinders cast together
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F7/00—Casings, e.g. crankcases or frames
    • F02F7/0002—Cylinder arrangements
    • F02F7/0007—Crankcases of engines with cylinders in line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F2200/00—Manufacturing
    • F02F2200/06—Casting
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/4927—Cylinder, cylinder head or engine valve sleeve making

Definitions

  • the present invention relates to a process for producing a cylinder block of an engine. More particularly, the present invention relates to a process for producing a cylinder block in which the intervals between the cylinder bores are narrow and cooling water passages are formed between the cylinder bores.
  • a cylinder block having a plurality of cylinder bores has been conventionally employed in a common engine.
  • a cylinder head is attached with a gasket to a sealing surface of the cylinder block.
  • a water jacket is formed to surround all of the cylinder bores, and cooling water is allowed to flow through the jacket. Since the cylinder bores are heated to a high temperature by the heat of combustion, generated when a gaseous mixture is combusted, it is essential that the cylinder bores are cooled around the periphery. For such purpose, it is preferred to provide a cooling water passage between the cylinder bores and to distribute cooling water to such passages as well as to the water jacket described above. However, in a cylinder block having relatively thin walls between the bores, it is difficult to form cooling water passages between the cylinder bores.
  • Japanese Unexamined Patent Publication No. 61-209763 discloses a process for producing a cylinder block, in which a plurality of cylinder liners are arranged in a mold with a pipe located between each adjacent pair of cylinder liners. These liners and pipes are permanently embedded in molten metal put into the mold. Thus, cylinder bores and cooling water passages are defined by the inner circumferential surfaces of the cylinder liners and the pipes, respectively.
  • slit-shaped grooves are defined between adjacent cylinder bores on the sealing surface of the cylinder block so as to constitute the interbore cooling water passages.
  • holes communicating with the water jacket are formed between the cylinder bores using a tool such as a drill to constitute the interbore cooling water passages. Such holes are usually referred to as drill paths.
  • the cylinder liners should have a wall thickness of about 2 mm for adequate strength. If cylinder liners having such thickness are arranged such that the bore-to-bore intervals are 5 to 6 mm, the intervals between the outer circumferences of each two adjacent cylinder liners will be 1 to 2 mm. Meanwhile, the pipe should have a passage with a diameter of at least 1 mm so that the cooling water may pass through it. Accordingly, it is difficult to arrange pipes having passages with such diameter and to embed them by casting.
  • interbore cooling water passages are defined by slit-shaped grooves
  • the width of the sealing surface between the cylinder bores will be small.
  • the contact area between the sealing surface and the gasket is small, and this results in an inadequate seal.
  • drill paths constitute the interbore cooling water passages
  • the present invention was accomplished in view of the circumstances as described above, and it is an objective of the present invention to provide a cylinder block having interbore cooling water passages through which a sufficient amount of water can be distributed even when the bore-to-bore distance is small. Furthermore, a sealing surface with a sufficient seal area is achieved.
  • a method comprises the step of providing a plurality of cylinder liners, each having one of said cylinder bores and at least one connecting portion.
  • a liner assembly is formed by joining said cylinder liners at their connecting portions. At least one of the connecting portions has a recess that forms a space located between the cylinder bores when the connecting portions are joined.
  • the liner assembly is positioned in a mold.
  • a cast body having said water jacket around said liner assembly is molded by pouring molten metal into the mold. The space is blocked to prevent said molten metal from entering the space during molding.
  • a cylinder block can be produced.
  • the cylinder block has a sealing surface on which a gasket is mounted.
  • the cylinder bores are arranged side by side. Each cylinder bore opens to said sealing surface.
  • the water jacket surrounds said cylinder bores, and the cooling passage is located between the cylinder bores.
  • FIGS 8 and 9 show a cylinder block 11 for a four-cylinder engine produced according to the process of the present invention.
  • the cylinder block 11 comprises a block main body 12, a liner assembly 14, a water jacket 16 and interbore cooling water passages 17.
  • the block main body 12 is made of aluminum and is molded by means of die casting, medium-pressure molding, low-pressure molding, or the like.
  • the block main body 12 is formed to have a flat upper face to provide a sealing surface 13 on which a gasket 63 (to be described later) is placed.
  • the liner assembly 14 contains a group of four cylinder bores, and the assembly 14 is embedded in the block main body 12 as shown in Fig. 9.
  • the water jacket 16 provides a passage for cooling water 19 for cooling the block main body 12 and the liner assembly 14 and is formed around the liner assembly 14 so as to surround the group of cylinder bores.
  • the interbore cooling water passages 17 are defined so as to introduce the cooling water 19 in the water jacket 16 between the cylinder bores.
  • the interbore cooling water passages 17 comprise three closed spaces 21, 22 (only two spaces are shown in Figure 8) defined at the top of the liner assembly 14 between adjacent cylinder bores and between communicating holes 23, 24, which connect the closed spaces 21, 22 to the water jacket 16.
  • the closed spaces 21, 22 each has a flat rectangular form, and the upper extremity of each space is positioned to be spaced downward from the upper end 15 of the liner assembly 14.
  • the holes or passages 23, 24 are open at their tops to the sealing surface 13 of the block main body 12, at their bottoms to the closed spaces 21, 22 and at their sides to the water jacket 16.
  • the cylinder bore group comprises a first cylinder bore #1, a second cylinder bore #2, a third cylinder bore #3 and a fourth cylinder bore #4.
  • Each of the cylinder bores #1, #2, #3, #4 is directed to accommodate a piston 26 having piston rings 25 such that the piston 26 may move reciprocally.
  • the adjacent cylinder bores #1 to #4 are arranged to be spaced from one another at very close intervals of 5 to 6 mm.
  • the upper space defined by the piston 26 in each cylinder bore #1 (#2, #3, #4) constitutes a part of combustion chamber 27 in which a gaseous mixture of fuel and air is burnt.
  • Each of the cylinder bores #1 to #4 has a cylindrical surface with high accuracy (roundness) so as to form a proper seal against the gaseous mixture and the gas generated by combustion.
  • the liner assembly 14 is constituted by arranging a first cylinder liner 31, a second cylinder liner 32, a third cylinder liner 33, and a fourth cylinder liner 34 in a line and interconnecting adjacent cylinder liners 31 through 34.
  • These cylinder liners 31 through 34 are formed of aluminum alloy, as will be described later.
  • the first and fourth cylinder liners 31 and 34 positioned on the opposite ends are of the same shape, and the intervening second and third cylinder liners 32 and 33 are of the same shape.
  • the fourth cylinder liner 34 is rotated 180° with respect to the first cylinder liner 31, and the third cylinder liner 33 is rotated 180° with respect to the second cylinder liner 32.
  • the four-part liner assembly 14 is constituted by just two cylinder liner shapes.
  • the first and fourth cylinder liners 31 and 34 have a generally cylindrical shape, and their inner peripheral surfaces form the first and fourth cylinder bores #1 and #4, respectively.
  • Each of the cylinder liners 31 and 34 is provided with a single connecting portion 35 extending outward and having a flat joining surface 36 at its end portion.
  • the second and third cylinder liners 32 and 33 are in a generally cylindrical shape, and their inner peripheral surfaces form the second and third cylinder bores #2 and #3, respectively.
  • Each of the cylinder liners 32 and 33 is provided with a pair of connecting portions 37 and 39 protruding from opposite sides of each cylinder liner and having flat joining surfaces 38 and 41 at their end portions.
  • a pair of grooves 42 are formed to extend along the overall length of the cylinder liners 31 and 34.
  • a pair of tongues 43 are formed to extend along the overall length of the cylinder liners 32 and 33.
  • a single groove 44 and a single tongue 46 are formed, one on each side, to extend along the overall length of the cylinder liners 32 and 33.
  • the tongues 43 and 45 and grooves 42 and 44 are formed so that a set of conditions are established. Referring to Figure 3, the depth of the groove 42 (or 44) is H1, the width is W1, the height of the tongue 43 (or 45) is H2, and the width is W2. The conditions are: H1 > H2 and W1 ⁇ W2
  • W1 ⁇ W2 is a necessary condition for the tongues 43 and 45 to be press-fitted into the grooves 42 and 44 to connect the cylinder liners 31 through 34 together.
  • H1 > H2 is a necessary condition for the joining surfaces 36, 38, and 41 to be closely contacted with each other when adjacent cylinder liners 31 through 34 are connected.
  • both of the joining surfaces 36 and 38 are shifted from an imaginary plane L2, passing halfway between the cylinder bores #1 and #2, toward the first cylinder bore #1 by half of the width L of the interbore cooling water passage 17 (closed space 21).
  • both of the joining surfaces 36 and 38 are shifted from an imaginary plane, passing halfway between the cylinder bores #4 and #3, toward the fourth cylinder bore #4 by half of the width L.
  • both of the joining surfaces 41 and 41 are positioned on an imaginary plane L1 passing halfway between the cylinder bores #2 and #3.
  • recess portions 47 with a depth D/2 are provided between each groove 44 and the tongue 45 on the opposite side.
  • the closed space 22 with a width L is formed by both recess portions 47 and 47.
  • the combustion heat has lesser effect on the cylinder liner, and consequently, the lower portion can be sufficiently cooled by the cooling water 19 flowing through the water jacket 16.
  • the lower portion of the liner 14 does not always require the interbore cooling water passages 17.
  • the aluminum cylinder liners 31 through 34 normally require the following characteristics (1) through (3):
  • the liner is made from base powder obtained by quench hardening and by using powder metallurgy based on hot plastic working. This results in superior characteristics such as low thermal expansion, high wear resistance, high thermal resistance and mechanical properties equal to steel or cast-iron, unlike liners made by a conventional casting elongation method.
  • the liner material is formed by dispersing ceramic particles such as alumina (Al 2 O 3 ) particles and graphite powder in a matrix including silicon (Si) powder, iron (Fe) powder, copper (Cu) powder, magnesium (Mg) powder, manganese (Mn) powder, nickel (Ni) powder and aluminum (Al) powder.
  • ceramic particles such as alumina (Al 2 O 3 ) particles and graphite powder in a matrix including silicon (Si) powder, iron (Fe) powder, copper (Cu) powder, magnesium (Mg) powder, manganese (Mn) powder, nickel (Ni) powder and aluminum (Al) powder.
  • silicon is added for enhancing wear resistance
  • iron is added for enhancing heat resistance
  • Alumina is added for enhancing wear resistance
  • graphite is added for burning resistance.
  • the liner has an outer layer formed of an expanded material of aluminum alloy.
  • This process includes a step of forming the liner assembly 14, a step of molding a cast body 62 and a step of forming the communicating passages (holes 23 and 24).
  • the cylinder liners 31 through 34 are made first.
  • the matrix powder comprising the aforementioned materials, alumina, and graphite are homogeneously mixed, and a cylindrical billet is molded by cold isostatic press (CIP).
  • CIP cold isostatic press
  • the billet is inserted into a can made of aluminum alloy to produce a composite billet.
  • This composite billet is inserted into a mold for molding a cylinder liner, and an elongated material is extruded and molded while applying heat and pressure.
  • metallic bonding occurs between powders, and also the elongated material of two-layer structure having tongues 43 and 45 and/or grooves 42 and 44 at the outer layer is obtained.
  • the tongues 43 and 45 or grooves 42 and 44 are formed by extrusion, and consequently, there is no need for forming these later. If the elongated material is cut at a predetermined length and then the recess portions 46 and 47 are formed in the outer layer by a cutting operation, the cylinder liners 31 through 34 will be obtained as shown in Figure 1.
  • each of the connecting portions 35 of the first and fourth cylinder liners 31 and 34 is designed to have a pair of the grooves 42.
  • One connecting portion 37 of she second and third cylinder liners 32 and 33 has a pair of the tongues 43, while the other connection portion 39 has a single groove 44 and a single tongue 45. That is, the first and fourth cylinder liners 31 and 34 are formed into the same shape, and the second and third cylinder liners 32 and 33 are formed into the same shape. For this reason, the components can be used in common, and four cylinder liners 31 through 34 can be prepared by making only the aforementioned two kinds of cylinder liners.
  • the four cylinder liners 31 through 34 are interconnected to form the liner assembly 14. More specifically, adjacent cylinder liners 31 through 34 are connected to each other and the tongues 43 and 45 are press fitted into the corresponding grooves 42 and 44. When this occurs, adjacent joining surfaces 36 and 38 and adjacent joining surfaces 41 and 41 are brought into contact with each other by the aforementioned press fitting because the grooves 42 and 44 are formed more deeply than the height of the tongues 43 and 45 (H1 > H2). Since the grooves 42 and 44 are formed narrower than the width of the tongues 43 and 45 (W1 ⁇ W2), adjacent cylinder liners 31 through 34 are interconnected with an extremely small or non-existant gap therebetween.
  • the closed spaces 21 and 22 are formed between adjacent cylinder liners 31 through 34. That is to say, between the first and second cylinder liners 31 and 32, the closed space 21 is formed by the joining surface 36 and the recess portion 46. Likewise, between the fourth and third cylinder liners 34 and 33, the closed space 21 is formed by the joining surface 36 and the recess portion 46. Furthermore, between the second and third cylinder liners 32 and 33, the closed space 22 is formed by a pair of the recess portions 47. These closed spaces 21 and 22 all have the same volume and also each closed space is located halfway between adjacent cylinder bores #1 to #4. In this way, the liner assembly 14 with three closed spaces 21, 22, and 21 is made.
  • a mold 48 shown in Figure 5 is used.
  • This mold 48 is provided with a stationary mold 49, an upper movable mold 51, a lower movable mold 52, a side movable mold 53, and a core mechanism 54.
  • a plurality of small diameter holes 55 and large diameter holes 56 are bored in the stationary mold 49 at a plurality of places, and each small diameter hole 55 is continuous with an associated one of the large diameter holes 56.
  • a protruding portion 57 for forming the water jacket 16 is provided on the side surface 50 of the stationary mold 49 around each large diameter hole 56.
  • the upper movable mold 51 is disposed above the protruding portion 57, while the lower movable mold 52 is disposed under the protruding portion 57. Both movable molds 51 and 52 vertically reciprocate while sliding on the side surface 50 of the stationary mold 49. Thus, the movable molds 51 and 52 are moved toward and away from the protruding portion 57.
  • the side movable mold 53 is located so that it can horizontally reciprocate, and with this reciprocal motion, the side movable mold 53 is moved toward and away from the stationary mold 49.
  • the core mechanism 54 is provided with rods 58 corresponding in number to the cylinder bores #1 through #4 and a plurality of core pieces 59 located around each rod 58.
  • Each rod 58 is inserted into the large diameter hole 56 and small diameter hole 55 so that it can reciprocate with respect to the stationary mold 49.
  • the distal end portion (left end portion in Figure 5) of the rod 58 is formed so that its diameter is gradually reduced toward the side movable mold 53.
  • the core pieces 59 are formed into an elongated shape and are located within the protruding portion 57 and the large diameter hole 56 so that they form an annular shape around the rod 58.
  • each core 59 is tapered so that the thickness of each core piece is reduced toward the stationary mold 49, and the inner peripheral surface is held in contact with the outer peripheral surface of the rod 58. Therefore, with longitudinal motion of the rod 58, if the contacting portion, between the rod 58 and the core pieces 59, is varied, the opposing core pieces 59 will be moved (or expanded) so that the interval between the core pieces is increased, or moved (or contracted) so that the interval is reduced. Note that, when the core pieces 59 are maximally expanded, they are brought into contact with the inner peripheral surface of the large diameter hole 56.
  • the liner assembly 14 is cast in aluminum by using the mold 48, first, the three movable molds 51 to 53 are moved away from the protruding portion 57, and all the rods 58 are retracted so that the core pieces 59 are contracted, as shown in Figure 5. Then, the liner assembly 14 is inserted into the protruding portions 57 so that the core pieces 59 are allowed to enter the cylinder liners 31 through 34. Because the core pieces 59 have been contracted, they readily enter the cylinder bores #1 through #4.
  • the three movable molds 51 to 53, as shown in Figure 6, are moved so that they are close to the protruding portion 57. If the molds are thus clamped, a cavity 61 for molding the block body 12 will be formed between the stationary mold 49, the movable molds 51 to 53, and the liner assembly 14. Molten metal is injected into this cavity 61.
  • the liner assembly 14 is formed by bonding the connecting portions 35, 37, and 39 of the cylinder liners 31 through 34 together, a gap tends to occur between adjacent connecting portions 35 and 37 and between adjacent connecting portions 39 and 39. It is possible that molten metal will enter the gaps and get into the recess portions 46 and 47. However, as shown in Figures 4 and 13, the tongues 43 and 45 are press fitted into the grooves 42 and 44 along the entire length of the connecting portions 35, 37, and 39, and the gap between the groove and the tongue is substantially zero. For this reason, the molten metal is prevented from passing from the side of the liner assembly 14 through the gaps and getting into the recess portions 46 and 47.
  • the gap between the joining surfaces 36 and 38 and between the joining surfaces 41 and 41 is so small that it can be neglected, even at places other than the tongues 43 and 45 or grooves 42 and 44. For this reason, the molten metal can be prevented from passing from the top or bottom of the liner assembly 14 through the gaps and getting into the recess portions 46 and 47.
  • a set of cores of the type where the diameter of the core set is slightly smaller than that of the cylinder bores and cannot be varied is used instead of the core mechanism 54, a gap occurs between the cylinder bores #1 through #4 and the cores and high pressure is applied from the outside on the liner assembly 14 when casting. Therefore, there is possibility that the liner assembly 14 may become deformed toward the core set. If such deformation occurs, it is possible that the core set cannot be pulled out from the liner assembly 14 after casting.
  • the core pieces 59 of the core mechanism 54 are expanded and contacted with the cylinder bores #1 through #4 with pressure, there is no gap between each core and the cylinder bore, or even if there were a gap, it would be small. For this reason, even if the molten metal shrinks while solidifying and applies force to the liner assembly 14 from the outside, that force would be received by each core piece 59 and the rod 58 and deformation would be prevented. Also, even if the liner assembly 14 were deformed, the core pieces 59 could be moved away from the cylinder bores #1 through #4, i.e., the cast body 62, because the rods 58 are tapered.
  • the interbore cooling water passage 17 In manufacturing the cylinder block 11, no pipe is used for forming the interbore cooling water passage 17, unlike the prior art. By eliminating the pipe, it is possible to enlarge the width L of the interbore cooling water passage 17. In addition, because part of the interbore cooling water passage 17 is constituted by the closed spaces 21 and 22, the area that the interbore cooling water passage 17 occupies on the sealing surface 13 is smaller. Therefore, as compared with the prior art where slit grooves are formed, the area of the sealing surface 13 between each of the cylinder bores #1 through #4 is greater. Furthermore, by forming the recess portions 46 and 47 constituting the closed spaces 21 and 22 with a suitable size, it is possible to form the interbore cooling water passage 17 with a volume larger than that of a drill path bored by a conventional drill.
  • a cylinder head 64 is assembled on the cylinder block 11 through a gasket 63, and an oil pan (not shown) is secured to the lower surface of the cylinder block 11.
  • air-fuel mixture is burnt in the combustion chamber 27, and the walls of the combustion chamber 27, that is, the cylinder liners 31 through 34 reach a high temperature.
  • the cooling water 19 flows through the water jacket 16, and some of the cooling water 19 flows through the interbore cooling water passage 17. Heat is transferred between the high-temperature cylinder liners 31 through 34 and the cooling water 19, and the cylinder liners 31 through 34 are cooled.
  • Each interbore cooling water passage 17 is positioned halfway between adjacent cylinder bores #1 through #4, and the distances from the cylinder bores #1 through #4 to the respective interbore cooling water passages 17 are equal to one another. For this reason, the adjacent cylinder liners 31 through 34 are equally cooled by the cooling water 19 flowing through the cooling water passages 17.
  • the cylinder bores #1 through #4 are cooled about their entire peripheries. At this time, because the interbore cooling water passage 17 has a large volume, as described above, the cylinder bores #1 through #4 are cooled more effectively than with the prior art designs where the interbore cooling water passages are formed by a drill.
  • each of the cylinder bores #1 through #4 is held to a cylindrical shape having a circular opening, that is, the bore can be held to a high degree of roundness.
  • the piston ring 25 satisfactorily follows the reciprocal motion of the piston 26, a gap is hardly generated between the ring 25 and each of the cylinder bores #1 through #4, and that engine oil hardly passes through this gap and hardly gets into the combustion chamber 27.
  • this invention achieves high sealing performance because the liner assembly 14 is buried in the block body 12 and the sealing surface of the block body 12 is formed flat. That is, if the liner assembly 14 is constructed so that the top surface 15 thereof is exposed, a boundary line will be exposed between the top surface 15 and the top surface of the block body 12. These top surfaces function as a sealing surface for sealing the gasket 63.
  • the liner assembly 14 and the block body 12 are formed of different materials having different linear expansion coefficients. Thus, even if the top surface 15 of the liner assembly 14 and the top surface of the block body 12 are initially positioned on the same plane, a step portion would be formed between both top surfaces when both the liner assembly 14 and the block body 12 are heated due to the operation of the engine. This will cause a gap between the step portion and the gasket 63, and sealing performance will be reduced.
  • the liner assembly 14 is buried in the block body 12, and the sealing surface 13 is constituted only by the top surface of the block body 12. For this reason, even when the thermal expansion differs between the liner assembly 14 and the block body 12 because of the difference between the liner expansion coefficients, a good seal is achieved because the sealing surface 13 is flat with no step.
  • the entire length of the cylinder block 11 (length in the direction of the array of the cylinder bores #1 through #4) is short and the entire length of the engine becomes short. For this reason, the weight of the engine is reduced and the mounting flexibility on a vehicle is enhanced.
  • the cylinder is formed of aluminum
  • the inner surface of the cylinder bore is plated with nickel
  • a metal matrix composite (MMC) layer is formed inside the cylinder bore
  • a high-silicon aluminum alloy (A390) is etched, in order to improve the sliding characteristics between the piston and the piston ring.
  • the cylinder is manufactured with low-pressure casting and low-speed and intermediate-pressure casting, but as compared with a die-cast method, the average thickness is great, the entire cylinder block is heavy, and the casting cycle is long.
  • a groove 65 for applying an adhesive agent is provided in either a joining surface 36 or a joining surface 38, or in one of the adjacent joining surfaces 41.
  • the groove 65 as shown in Figure 15, comprises a main portion 66 formed into a rectangular shape along the peripheral margin of the joining surface 38 (36, 41) and a straight partition 67 extending along the lower edge of a recess portion 46 (47) and connected to the main portion 66.
  • this embodiment has the same operation and advantages as the first embodiment, and in addition, the adhesive agent and the groove 65 both function to bond the connecting portions 35, 37, and 39 and to seal against molten metal.
  • the grooves 42 and 44 or the tongues 43 and 45 in the first embodiment can be omitted.
  • each of the joining surfaces 36, 38, and 41 has a very flat, smooth surface like a mirror, except for the recess portions 46 and 47.
  • a mold with a pair of pins 71 and 72 is used. The pins 71 and 72 are arranged so that they can move back and forth longitudinally.
  • both pins 71 and 72 are moved outward from the mold, and cylinder liners 31 through 34 are arranged in a line and are placed within the mold.
  • the pin 71 is moved inward so that the first cylinder liner 31 is pushed toward the second cylinder liner 32.
  • the pin 72 is moved inward so that the fourth cylinder liner 34 is pushed toward the third cylinder liner 33.
  • Adjacent joining surfaces 36 and 38 contact each other with pressure, and adjacent joining surfaces 41 are contacted with each other with pressure, whereby the liner assembly 14 is formed.
  • molten metal is injected into the mold and a cast body 62 is molded. After the molten metal solidifies, both the pins 71 and 72 are retracted and the cast body 62 is taken out from the mold 48.
  • Holes 73 are produced in the cast body 62 by the pins 71 and 72. Since these holes 73 communicate the water jacket 16 with the outer surface of the cast body 62, they are closed with plugs (not shown) after the cast body 62 is taken out.
  • the third embodiment is identical with the first and second embodiments and therefore further description is omitted. Therefore, this embodiment has the same operation and advantages as the first and second embodiments, and in addition, the grooves 42 and 44, the tongues 43 and 45, and the groove 65 are unnecessary. In addition, the operation of applying an adhesive can be omitted.
  • This embodiment differs in the shape of the connecting portions 35, 37, and 39 of the cylinder liners 31 through 34, the formation process of the liner assembly 14, and the molding process of the cast body 62.
  • connecting portions 35 and 37 of the first and second cylinder liners 31 and 32 are used as an example, the same may be applied to the other connecting portions.
  • a pair of grooves 42 are formed in the side portions of the joining surface 36 of the first cylinder liner 31.
  • a pair of clamping tongues 80 and 81 are integrally formed at both sides of each groove 42 of the joining surface 36.
  • the distal end of each clamping tongue 80 (81) is provided with a bulged portion 82 (83) extending toward the opposing clamping tongue 81 (80).
  • a pair of tongues 43 is provided extending along the entire height of the cylinder liner 32.
  • the tongues 43 are provided by forming grooves 84 in the connecting portion 37.
  • the tongue 43 includes a main portion 85 and a head portion 86 positioned at the distal end.
  • the width W3 of the main body portion 85 is set so that it is narrower than the distance d between the bulged portions 82 and 83.
  • the width W4 of the head portion 86 is set so that it is wider than the distance d and narrower than the width W1 of the groove 42. Therefore, the tongue 43 can be fitted into the groove 42 by press fitting the head portion 86 between the bulged portions 82 and 83.
  • the distal end of the head portion 86 is located on nearly the same plane as the joining surface 38.
  • a pair of fittings 87 (Fig. 20) is constituted by the grooves 42, 84, the clamping tongues 80 and 81, and the tongue 43.
  • the location of the fittings 87, as shown in Figure 22, is where the holes 23 and 24 are bored in the process of forming the communicating passages.
  • the shape or size of the grooves 42 and 84 is made so that spaces 88 and 89 into which molten metal can flow are formed in the vicinity of the fitting 87 between the connecting portions 35 and 37, when the head 86 is fitted into the groove 42 as shown in Figure 21.
  • One space 88 is surrounded and formed by the wall surfaces of both clamping tongues 80 and 81, head portions 86, and groove 42, when the head portion 86 is press fitted up to the limit (when joining surfaces 36 and 38 contact each other and further press fitting of head portion 86 is regulated).
  • the other space 89 is surrounded and formed in the same manner by the wall surfaces of one clamping tongue 80, tongue 43, and groove 84.
  • These spaces 88 and 89 are required to have a width of 0.2 mm or more in view of the flowability of molten metal. If the width is narrower than 0.2 mm, molten metal (aluminum for this case) may not sufficiently flow into the spaces 88 and 89.
  • first and second cylinder liners 31 and 32 are moved toward each other, as shown by arrows in Figures 18 and 19.
  • the head portion 86 of the tongue 43 is brought into contact with the distal ends of the corresponding clamping tongues 80 and 81.
  • the head portion 86 is press fitted between the bulged portions 82 and 83 having the distance d narrower than the width W4 of the head portion 86. If the major part of the head portion 86 is pressed in until passing through both bulged portions 82 and 83, both joining surfaces 36 and 38 will be in contact with each other.
  • both connecting portions 35 and 37 are thus fitted at the fittings 87, adjacent cylinder liners 31 and 32 will be bonded with each other, as shown in Figures 20 and 21.
  • the liner assembly 14 is formed with the closed space 21 between both connecting portions 35 and 37 and also has, at two places in the fittings 87, the spaces 88 and 89 into which molten metal can flow.
  • the liner assembly 14 is used as an insert. This insert is arranged in the predetermined position within the mold 48 shown in Figure 5, and metal in the molten state is pressurized to a predetermined pressure and is injected into the cavity. Part of the injected molten metal flows into the two spaces 88 and 89. The molten metal gets into the spaces 88 and 89 with reliability because both spaces 88 and 89 are sufficiently large (0.2 mm across or more). Then, when the molten metal, filled in the spaces 88 and 89, is cooled and solidified, and, as shown in Figure 23, the cast body 62 will be formed, which has the water jacket 16 surrounding the liner assembly 14. Thereafter, this cast body 62 is taken out from the mold 48.
  • holes 23 and 24 are bored in the places corresponding to both sides of the joining surfaces 36 and 38 of the connecting portions 35 and 37 of the liner assembly 14, that is, through the fittings 87 from the top of the cast body 62 by a boring tool such as a drill. Then, the sides of the closed space 21 and the water jacket 16 are communicated with each other by the holes 23 and 24.
  • the interbore cooling water passage 17 is formed by the closed space 21 and the holes 23 and 24, and the desired cylinder block 11 made of aluminum is obtained.
  • first, second, and third embodiments are entirely different from the first, second, and third embodiments with respect to the shape of the recess portion and the method of forming the interbore cooling water passage 17. While the first and second cylinder liners 31 and 32 are used in the following discussion for convenience, the same may be applied to the cylinder liners 33 and 34.
  • a plurality of grooves 92 extending from one side surface 37a of a connecting portion 37 to the other side surface 37b are provided in the upper portion (right portion in Figure 25) of the joining surface 38 of the second liner 32.
  • three grooves 92 crossing the axis L3 of the second cylinder liner 32 are shown in Figure 25.
  • the recess portion is constituted by these grooves 92.
  • This method is comprised of a process of forming the liner assembly 14, a process of arranging the liner assembly 14 in the mold 48, a process of molding the cast body 62, and a process of forming the water jacket 16 and the interbore cooling water passage 17.
  • the cylinder liners 31 and 32 are first made as shown in Figure 24.
  • Matrix powder, alumina, and graphite, described in the first embodiment, are homogeneously mixed, and a billet with holes is formed by CIP.
  • the billet is inserted into a can made of aluminum alloy to produce a composite billet, and the temperature of the billet is raised by applying heat.
  • This composite billet is inserted into a mold and is extruded with pressure.
  • metallic bonding occurs between powders, and an elongated material of two-layer structure is obtained.
  • the elongated material is cut to a predetermined length, and then a cutting operation is applied to the outer layer.
  • the second cylinder liner 32 having three grooves 92 at the top of its joining surface 38 is obtained as shown in Figure 24.
  • the first cylinder liner 31 is molded.
  • the cylinder liners 31 and 32 are connected to form the liner assembly 14.
  • the method of press fitting a tongue into a groove (the first embodiment)
  • the method of using an adhesive between connecting portions (the second embodiment)
  • the method of contacting cylinder liners together by pins (the third embodiment) can be used.
  • this mold 48 basically similar to the first embodiment, is equipped with a stationary mold 49, an upper movable mold 51, a lower movable mold 52, a side movable mold 53, and a core mechanism 54.
  • a protruding portion 57 for forming the water jacket 16 comprises a thick portion 57a and a distal end portion 57b.
  • the distance d1 of the thick portion 57a is set so as to be slightly smaller than the width (distance between side surfaces 37a and 37b) W5 of the connecting portion 37, and the distance d2 of the distal end portion 57b is made larger than the width W5.
  • the core mechanism 54 is equipped with a plurality (same number as the numbers of cylinders) of core pins 94 protruding from the stationary mold 49 toward the side movable mold 53.
  • Each core pin 94 is formed in a round bar shape having a diameter slightly smaller than the cylinder bore #1 (#2).
  • a plurality of pins 95 are provided on the outside of the protruding portion 57.
  • Each bolt hole 96 is a hole into which a bolt is screwed for securing the cylinder head 64 to the cylinder block 11.
  • the mold 48 In order to arrange the liner assembly 14 in the mold 48, first the three movable molds 51 to 53 are moved away from the molded protruding portion 57, and the mold 48 is opened as shown in Figure 25.
  • the cylinder liner 32 (31) of the liner assembly 14 is put over the corresponding core pin 94 and is pushed as far as the position shown in Figure 26. This position is the position where the connecting portion 37 (35) starts contacting the thick portion 57a when the liner assembly 14 is pushed in.
  • the process of forming the cast body 62 is as follows. In this process, molten metal is injected into the aforementioned cavity 61. At this time, the connecting portions 35 and 37 have been bonded together and the gap between the joining surfaces 36 and 38 is substantially zero. In addition, the ends of all the through passages 93 have been closed by the thick portion 57a. Thus, molten metal is prevented from getting into all the through passages 93.
  • the cast body 62 having the liner assembly 14, the water jacket 16 surrounding the liner assembly 14 and the plurality of bolt holes 96 positioned outside the water jacket 14, cast in that metal (aluminum), will be formed as shown in Figure 28.
  • the interbore cooling water passage 17, through which a sufficient amount of cooling water can pass, is formed although the interval between the cylinder bores #1 and #2 is small.
  • a sufficient sealing surface 13 area is obtained between the cylinder bores #1 and #2.
  • the liner assembly 14, where the opposite ends of the through passages 93 are open at the side surfaces 37a and 37b of the connecting portion 37, is formed, and the opening is closed or opened by part of the mold 48 (protruding portion 57). Accordingly, there is no need for cutting out part of the cast body 62 for forming the interbore cooling water passage 17 after molding of the cast body 62. The number of manufacturing steps is reduced and the manufacturing cost of the cylinder block 11 is reduced.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
EP96106912A 1995-05-26 1996-05-02 Procédé pour la production de blocs-moteurs Expired - Lifetime EP0744541B1 (fr)

Applications Claiming Priority (9)

Application Number Priority Date Filing Date Title
JP128513/95 1995-05-26
JP12851395 1995-05-26
JP12851395 1995-05-26
JP27136995 1995-10-19
JP27136995 1995-10-19
JP271369/95 1995-10-19
JP5805696 1996-03-14
JP8058056A JPH09170487A (ja) 1995-05-26 1996-03-14 シリンダブロックの製造方法
JP58056/96 1996-03-14

Publications (2)

Publication Number Publication Date
EP0744541A1 true EP0744541A1 (fr) 1996-11-27
EP0744541B1 EP0744541B1 (fr) 1999-07-14

Family

ID=27296469

Family Applications (1)

Application Number Title Priority Date Filing Date
EP96106912A Expired - Lifetime EP0744541B1 (fr) 1995-05-26 1996-05-02 Procédé pour la production de blocs-moteurs

Country Status (4)

Country Link
US (1) US5755028A (fr)
EP (1) EP0744541B1 (fr)
JP (1) JPH09170487A (fr)
DE (1) DE69603229D1 (fr)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0777043A1 (fr) * 1995-11-29 1997-06-04 Toyota Jidosha Kabushiki Kaisha Procédé de fabrication d'un bloc cylindre
WO1998040608A3 (fr) * 1997-03-12 1998-12-03 Pita Witehira Machine modulaire
EP0882534A1 (fr) * 1997-06-02 1998-12-09 Toyota Jidosha Kabushiki Kaisha Procédé pour la fabrication d'un bloc-cylindres d'un moteur à combustion interne
EP0863312A3 (fr) * 1997-03-07 1999-06-09 Thomas Industries, Inc. Assemblage de chemise de cylindre
DE19841102C1 (de) * 1998-09-09 2000-03-16 Daimler Chrysler Ag Kurbelgehäuse
DE10153720A1 (de) * 2001-10-31 2003-05-15 Daimler Chrysler Ag Zylinderkurbelgehäuse mit einer Zylinderlaufbuchse und Gießwerkzeug
WO2004015260A1 (fr) * 2002-08-06 2004-02-19 Peak Werkstoff Gmbh Combinaison de boites de glissement de cylindres en alliage leger
EP1440749A1 (fr) * 2002-12-17 2004-07-28 Bayerische Motoren Werke Aktiengesellschaft Procédé de fabrication d'un bloc-cylindres pour un moteur à combustion interne à refroidissement liquide
WO2005014205A1 (fr) * 2003-07-29 2005-02-17 Hottinger Maschinenbau Gmbh Procede et dispositif de positionnement de pieces metalliques a l'interieur ou a la surface de noyaux ou de moules de coulee
DE102004040539A1 (de) * 2004-08-20 2006-03-09 Audi Ag Zylinder-Kurbelgehäuse für eine Mehrzylinder-Hubkolbenmaschine
WO2008059329A1 (fr) * 2006-11-17 2008-05-22 Toyota Jidosha Kabushiki Kaisha Bloc cylindres et procédé de production de bloc cylindres
WO2008059330A1 (fr) * 2006-11-17 2008-05-22 Toyota Jidosha Kabushiki Kaisha Bloc-cylindres et procédé permettant de produire un bloc-cylindres
CN108252816A (zh) * 2016-12-28 2018-07-06 株式会社久保田 水冷发动机的冷却结构

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5873163A (en) * 1996-10-22 1999-02-23 Diefenthaler; Mark S. Method for repairing corroded cylinder castings in water-cooled engine blocks
EP1140407B1 (fr) * 1998-11-17 2004-01-21 Saab AB (publ) Usinage grande vitesse de materiau a matrice metallique
SE521289C2 (sv) * 1998-11-17 2003-10-21 Saab Ab Bearbetning av metalmatriskompositmaterial (MMC) medelst höghastighetsbearbetning (HSM)
IT1319899B1 (it) * 2000-02-10 2003-11-12 Fiat Ricerche Procedimento per la produzione di un blocco cilindri per un motore acombustione interna.
US20050150476A1 (en) * 2002-08-06 2005-07-14 Uwe Gohrbandt Combination of cylinder liners consisting of a light metal alloy
JP4185822B2 (ja) * 2003-06-25 2008-11-26 株式会社共立 内燃エンジン用シリンダの製造方法
US7559299B2 (en) * 2007-01-19 2009-07-14 Eastway Fair Company Limited Monolithic cylinder-crankcase
JP4187045B2 (ja) * 2007-03-16 2008-11-26 トヨタ自動車株式会社 シリンダブロック
US7814879B2 (en) * 2008-04-23 2010-10-19 Techtronic Outdoor Products Technology Limited Monolithic block and valve train for a four-stroke engine
US8191529B2 (en) * 2008-07-03 2012-06-05 Caterpillar Inc. Method of manufacturing an engine block
JP5381743B2 (ja) * 2010-01-22 2014-01-08 トヨタ紡織株式会社 樹脂製シリンダヘッドカバーの製造方法及び製造装置
JP5440206B2 (ja) * 2010-01-22 2014-03-12 トヨタ紡織株式会社 樹脂製シリンダヘッドカバーの製造方法及び製造装置
JP5853849B2 (ja) * 2012-03-08 2016-02-09 トヨタ自動車株式会社 レーザー溶接方法とエンジンの製造方法
US8875669B2 (en) 2012-04-27 2014-11-04 Ford Global Technologies, Llc Head gasket having variable area coolant openings
KR101509749B1 (ko) * 2013-11-27 2015-04-07 현대자동차 주식회사 실린더 블록을 구비한 엔진
BR102013031969A8 (pt) * 2013-12-12 2015-12-15 Mahle Int Gmbh camisa de cilindro de um motor a combustão interna
KR101637751B1 (ko) * 2014-12-01 2016-07-20 현대자동차주식회사 인터보어 집중 유량 공급형 워터 자켓이 적용된 알루미늄 모노 블록 엔진
US10113504B2 (en) * 2015-12-11 2018-10-30 GM Global Technologies LLC Aluminum cylinder block and method of manufacture
US10174707B2 (en) 2017-03-09 2019-01-08 Ford Global Technologies, Llc Internal combustion engine and method of forming
US10400707B2 (en) * 2017-07-26 2019-09-03 GM Global Technology Operations LLC Method and system for processing an automotive engine block

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3220775A1 (de) * 1982-06-02 1983-12-08 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart Zylinderkurbelgehaeuse fuer brennkraftmaschinen
US4469060A (en) * 1980-12-12 1984-09-04 Klockner-Humboldt-Deutz Aktiengesellschaft Gastight, undetachable connection of two metal parts
EP0356227A2 (fr) * 1988-08-23 1990-02-28 Honda Giken Kogyo Kabushiki Kaisha Système de refroidissement pour un moteur multicylindre
US5069266A (en) * 1989-01-19 1991-12-03 Mazda Motor Corporation Cylinder block making method and device

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59175649A (ja) * 1983-03-12 1984-10-04 Honda Motor Co Ltd 噛合伝動ベルト
JPS61209763A (ja) * 1985-03-14 1986-09-18 Fuji Heavy Ind Ltd シリンダブロツク
US4969263A (en) * 1989-04-18 1990-11-13 Tecumseh Products Company Method of making a cast engine cylinder having an internal passageway
US5232041A (en) * 1992-02-14 1993-08-03 Cmi International, Inc. Method for metallurgically bonding cast-in-place cylinder liners to a cylinder block
JPH05321751A (ja) * 1992-05-15 1993-12-07 Honda Motor Co Ltd 多気筒内燃機関用シリンダスリーブ集合体

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4469060A (en) * 1980-12-12 1984-09-04 Klockner-Humboldt-Deutz Aktiengesellschaft Gastight, undetachable connection of two metal parts
DE3220775A1 (de) * 1982-06-02 1983-12-08 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart Zylinderkurbelgehaeuse fuer brennkraftmaschinen
EP0356227A2 (fr) * 1988-08-23 1990-02-28 Honda Giken Kogyo Kabushiki Kaisha Système de refroidissement pour un moteur multicylindre
US5069266A (en) * 1989-01-19 1991-12-03 Mazda Motor Corporation Cylinder block making method and device

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0777043A1 (fr) * 1995-11-29 1997-06-04 Toyota Jidosha Kabushiki Kaisha Procédé de fabrication d'un bloc cylindre
US5732671A (en) * 1995-11-29 1998-03-31 Toyota Jidosha Kabushiki Kaisha Method and apparatus for manufacturing cylinder blocks
EP0863312A3 (fr) * 1997-03-07 1999-06-09 Thomas Industries, Inc. Assemblage de chemise de cylindre
US5970844A (en) * 1997-03-07 1999-10-26 Thomas Industries, Inc. Cylinder sleeve assembly
WO1998040608A3 (fr) * 1997-03-12 1998-12-03 Pita Witehira Machine modulaire
EP0882534A1 (fr) * 1997-06-02 1998-12-09 Toyota Jidosha Kabushiki Kaisha Procédé pour la fabrication d'un bloc-cylindres d'un moteur à combustion interne
DE19841102C1 (de) * 1998-09-09 2000-03-16 Daimler Chrysler Ag Kurbelgehäuse
DE10153720C2 (de) * 2001-10-31 2003-08-21 Daimler Chrysler Ag Zylinderkurbelgehäuse mit einer Zylinderlaufbuchse und Gießwerkzeug
DE10153720A1 (de) * 2001-10-31 2003-05-15 Daimler Chrysler Ag Zylinderkurbelgehäuse mit einer Zylinderlaufbuchse und Gießwerkzeug
WO2004015260A1 (fr) * 2002-08-06 2004-02-19 Peak Werkstoff Gmbh Combinaison de boites de glissement de cylindres en alliage leger
EP1440749A1 (fr) * 2002-12-17 2004-07-28 Bayerische Motoren Werke Aktiengesellschaft Procédé de fabrication d'un bloc-cylindres pour un moteur à combustion interne à refroidissement liquide
WO2005014205A1 (fr) * 2003-07-29 2005-02-17 Hottinger Maschinenbau Gmbh Procede et dispositif de positionnement de pieces metalliques a l'interieur ou a la surface de noyaux ou de moules de coulee
DE102004040539A1 (de) * 2004-08-20 2006-03-09 Audi Ag Zylinder-Kurbelgehäuse für eine Mehrzylinder-Hubkolbenmaschine
DE102004040539B4 (de) * 2004-08-20 2011-02-24 Audi Ag Zylinder-Kurbelgehäuse für eine Mehrzylinder-Hubkolbenmaschine sowie Verfahren zur Herstellung eines Zylinder-Kurbelgehäuses für eine Mehrzylinder-Hubkolbenmaschine
WO2008059329A1 (fr) * 2006-11-17 2008-05-22 Toyota Jidosha Kabushiki Kaisha Bloc cylindres et procédé de production de bloc cylindres
WO2008059330A1 (fr) * 2006-11-17 2008-05-22 Toyota Jidosha Kabushiki Kaisha Bloc-cylindres et procédé permettant de produire un bloc-cylindres
CN108252816A (zh) * 2016-12-28 2018-07-06 株式会社久保田 水冷发动机的冷却结构
CN108252816B (zh) * 2016-12-28 2021-07-02 株式会社久保田 水冷发动机的冷却结构

Also Published As

Publication number Publication date
US5755028A (en) 1998-05-26
DE69603229D1 (de) 1999-08-19
JPH09170487A (ja) 1997-06-30
EP0744541B1 (fr) 1999-07-14

Similar Documents

Publication Publication Date Title
EP0744541B1 (fr) Procédé pour la production de blocs-moteurs
US5732671A (en) Method and apparatus for manufacturing cylinder blocks
EP0554575B1 (fr) Bloc-cylindre
US20090000578A1 (en) Method for Making Cooling Channels in the Cylinder Head of an Internal Combustion Engine
US4570585A (en) Light metal cylinder head with valve seat insert
JP2007270813A (ja) 内燃機関用ピストン
US8176967B2 (en) Method for producing a cast component with a cast-in pipe
JP2007270812A (ja) 内燃機関用ピストン
CN109415994A (zh) 内燃机的制造方法、内燃机以及连接气缸
US5065714A (en) Heat-insulating structure of swirl chamber and its production method
US7392771B2 (en) Cylinder block and cylinder sleeve, method of producing cylinder block and cylinder sleeve by friction stir welding, and friction stir welding method
EP1052435A2 (fr) Support de segment de piston avec cavité de refroidissement et son procédé de fabrication
US4653161A (en) Manufacture process for aluminum alloy die-cast cylinders
JP3417331B2 (ja) シリンダヘッド及びその製造方法
US5016348A (en) Process for the manufacture of a tubular crankshaft
CN100429393C (zh) 发动机冷却液跨接件组件
EP0870919B1 (fr) Piston pour moteur à combustion interne et procédé pour sa fabrication
DE10235911B3 (de) Gussverbund von Hohlprofilen aus Leichtmetall-Legierung und Verfahren zu seiner Herstellung
US6439173B1 (en) Internal combustion engine with cylinder insert
US6925981B2 (en) Process for producing a cylinder block with a sleeve
US4969504A (en) Evaporable foam pattern for use in casting an exhaust manifold
EP0819836B1 (fr) Culasse et méthode pour fabriquer un siège de soupape
US6415848B1 (en) Metal mold arrangement for producing cylinder block
CZ100298A3 (cs) Odlitek ve formě bloku motoru a způsob jeho výroby
WO2020059371A1 (fr) Procédé de fabrication d'un piston pour moteur à combustion interne

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19960528

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

17Q First examination report despatched

Effective date: 19981019

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: THE PATENT HAS BEEN ANNULLED BY A DECISION OF A NATIONAL AUTHORITY

Effective date: 19990714

REF Corresponds to:

Ref document number: 69603229

Country of ref document: DE

Date of ref document: 19990819

ET Fr: translation filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 19991015

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20000502

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20000502